Airworthiness Directives 2004 - Revocation and Remaking - Beagle B121 (Pup) Series Aeroplanes

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Legislation au F2006B07735 In force Legislative Instrument

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Beagle B121 (Pup) Series Aeroplanes

 AD Name AD Number

 Fuel Tank Modification - CANCELLED AD/BEA 121/1

 Rudder Control Torque Tubes AD/BEA 121/2

 Engine Bearers AD/BEA 121/3

 Dual Throttle Control AD/BEA 121/4

 Rudder Control Lever Assembly P/N BE 45.10193 AD/BEA 121/5 Amdt 1

 Fuel Tank Non-Return Valves AD/BEA 121/6

 Elevator Torque Tubes AD/BEA 121/7 Amdt 1

 Rudder Control Torque Tubes AD/BEA 121/8 Amdt 3

 Bonding Points AD/BEA 121/9

 Rudder Drain Hole AD/BEA 121/10

 Fuel Tanks AD/BEA 121/11

 Front Seat Restraint Installation AD/BEA 121/12

 Internal Door Lock Operating Handle AD/BEA 121/13

 Fuselage/Mainplane Attachments AD/BEA 121/14 Amdt 3

 Flap Actuating Lever Assemblies AD/BEA 121/15

 Fuselage/Mainplane Attachments AD/BEA 121/16 Amdt 1

 Nosewheel Steering Mechanism AD/BEA 121/17

 Rudder Control Lever AD/BEA 121/18

 Rudder Pedal Anchorages AD/BEA 121/19

 Throttle Cable Assembly AD/BEA 121/20

 Nose Undercarriage and Rudder Control System AD/BEA 121/21

 Wing Spar Web AD/BEA 121/22 Amdt 1

 Engine Mounting Structure AD/BEA 121/23

 Fuselage Angle, Diaphragm and Flange at Tailplane Spar Attachments AD/BEA 121/24

 Control Rod End Fittings AD/BEA 121/25

 Rudder Control Tube Bolt AD/BEA 121/26

 Control Column Handgrips AD/BEA 121/27 Amdt 2

 Wing to Fuselage Main Spar Attachment Fitting AD/BEA 121/28

 Aircraft Fatigue Life AD/BEA 121/29

 Brake Torque Tube Assembly AD/BEA 121/30

 Main Spar Doubler at Main Landing Gear Attachment and Wing to Fuselage  AD/BEA 121/31 Amdt 1

 

Overview

The Airworthiness Directives 2004 is a legislative instrument that was enacted to update and streamline existing airworthiness directives pertaining to the maintenance and operation of specific aircraft types, in this case, Beagle B121 (Pup) Series Aeroplanes. This instrument was developed by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority (CASA), under the authority granted by subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary objective of this instrument is to revoke certain outdated airworthiness directives and re-make them in their most current form, ensuring that the regulations remain up-to-date and reflective of the latest safety standards. This was done to maintain the safety and airworthiness of the aircraft, thereby protecting the public and ensuring compliance with international aviation safety standards.

Scope and Application

The Airworthiness Directives 2004, promulgated by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, pertains to the aviation industry within Australia, focusing on the maintenance and safety of airworthy aircraft. This legislative instrument operates under the Civil Aviation Safety Regulations 1998 and specifically revokes and re-makes various airworthiness directives as listed in Schedule 1. These directives apply to the Beagle B121 (Pup) Series Aeroplanes, mandating compliance with specified modifications and maintenance actions to ensure the continued airworthiness of these aircraft. The geographic scope of this legislation is national, as it operates under the auspices of the Commonwealth and is applicable throughout Australia. Each Airworthiness Directive is reproduced verbatim from the latest published edition, ensuring that all industry stakeholders are subject to the same standards and requirements. The legislative instrument does not explicitly state exclusions or exemptions, and any further application or interpretation may be detailed in subordinate instruments.

Key Provisions

The Airworthiness Directives 2004 (F2006B07735) issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), includes two primary actions as outlined in section 2. Firstly, the Act revokes the Airworthiness Directives listed in Schedule 1, which encompass a range of modifications and amendments previously issued for the Beagle B121 (Pup) Series Aeroplanes (section 2(a)). Secondly, the Act re-makes each of these revoked Airworthiness Directives as separate instruments, ensuring that they are re-issued in the same form as the latest published editions (section 2(b)). This ensures that the regulatory framework for these aircraft remains current and enforceable. The obligations and requirements imposed by the Airworthiness Directives 2004 are significant for the entities and parties governed by the Act. For instance, owners and operators of Beagle B121 (Pup) Series Aeroplanes must comply with the specific modifications and maintenance requirements outlined in the re-made directives. These may include inspections, repairs, or replacements of various aircraft components such as rudder control torque tubes, engine bearers, and fuel tanks. Ensuring compliance with these directives is essential for maintaining the airworthiness of the aircraft and ensuring safety standards are met (sections 2 and Schedule 1). Failure to comply with the Airworthiness Directives 2004 can result in serious legal consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance with an Airworthiness Directive can be considered an offence. Penalties for breaching these directives can include fines and, in severe cases, criminal charges. The maximum penalties may vary depending on the nature and severity of the breach, but they are designed to enforce strict adherence to safety regulations. Ensuring that all aircraft maintain their airworthiness through compliance with these directives is crucial for the safety of all involved in aviation activities (sections 2 and 39.001(1) of the Civil Aviation Safety Regulations 1998).

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.